S 715-012
(3)
Do the operational test for the shutoff valve and the pneumatic actuator:
(a)
Start the APU (AMM 49-11-00/201).
(b)
During the APU operation, visually make sure the shutoff valve and the pneumatic actuator operate correctly.
(c)
Do the APU usual shutdown (AMM 49-11-00/201).
(4)
Close the access door 3701 for the stabilizer trim.
S 865-014
(5)
Remove the DO-NOT-CLOSE tag and close this circuit breaker:
S 415-013
(a) P6-2 Load Control Center Assembly
1) STABILIZER TRIM, CONT
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
49-51-21
ALL ú ú 01 Page 501 ú Nov 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / GTCP85-129 SERIES /737-300/400/500/ ENGINES/MAINTENANCE MANUAL ////////////////////////
TASK 49-51-21-705-001
3. Functional Test - Cooling Air Shutoff Valve (Fig. 501)
___________________________________________
A. Standard Tools and Equipment
(1) Pressurized Air Source - 7 psi (48 kPa) minimum
B. Access
(1)
Location Zones
101 Control Cabin (Left)
205 Electronic Compartment
701 Tail Compartment
(2)
Access Panels
1201 Electronic Equipment Access Door
3701 Stabilizer Trim Access Door
C. Procedure
S 865-002
(1)
Set the horizontal stabilizer trim in the full up position.
S 865-003
(2)
Set the switch and the circuit breakers:
(a)
Set the APU master switch on the P5 forward overhead panel to the OFF position and attach a DO-NOT-OPERATE tag.
(b)
Open these circuit breakers on the P6 Circuit Breaker Panel and attach the DO-NOT-CLOSE tags: 1) STABILIZER TRIM ACTUATOR 2) STABILIZER TRIM CONT 3) AUTO FLT CONT SYS B MACH TRIM AC 4) AUTO FLT CONT SYS B MACH TRIM DC 5) AFDS MCP CRS-2 6) AUTO FLT CONT SYS B SNSR EXC AC 7) AUTO FLT CONT SYS B FCC DC 8) AUTO FLT CONT SYS B ENGAGE INTLK B 9) AUTO FLT CONT SYS B WARN LIGHT BAT
(c)
Open these circuit breakers on the P18 Circuit Breaker Panel and attach the DO-NOT-OPERATE tags: 1) AUTO FLT CONT SYS A MACH TRIM AC 2) AUTO FLT CONT SYS A MACH TRIM DC 3) AFDS MCP DC 4) AIRPLANES WITH MECHANICAL AILERON FORCE LIMITER;
AFDS AIL FORCE LIM 5) AUTO FLT CONT SYS A SNSR EXC AC 6) AUTO FLT CONT SYS A FCC DC 7) AUTO FLT CONT SYS A ENGAGE INTLK A 8) AUTO FLT CONT SYS A WARN LIGHT BAT
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
49-51-21
ALL ú ú 01 Page 502 ú Nov 12/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
SEE A
FLIGHT COMPARTMENT
YOKE
STABILIZER
TRIM WHEEL
TRIM WHEEL CONTROL STAND
HANDLE
STABILIZER TRIM LOCK
A
Cooling Air Shutoff Valve - Adjustment/Test
Figure 501 (Sheet 1)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
49-51-21
ALL ú ú 01 Page 503 ú Nov 15/97
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
H00088
////////////////////////A / GTCP85-129 SERIES /737-300/400/500/ ENGINES /MAINTENANCE MANUAL ////////////////////////
SEE B
STABILIZER
JACKSCREW
STABILIZER TRIM
ELECTRICAL ACTUATOR ELECTRICAL
CONNECTOR
ELECTRICAL
CONNECTOR
AUTOPILOT STABILIZER TRIM SERVO
MANUAL TRIM DRIVE CABLE DRUM
B
Cooling Air Shutoff Valve - Adjustment/Test Figure 501 (Sheet 2)
H00091
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:737-300 400 500 AMM 飞机维护手册 AIRBORNE AUXILIARY POWER 2(67)